It is recognized, that mission requirements will play an even greater role in future military aircraft design. As these requirements become more stringent, the effective integration of aerodynamics, performance and control will be essential to meeting them. Specification of open loop airplane characteristics based on implied or indirect closed loop requirements will not be adequate. It appears knowledge of the pilot's dynamic and performance characteristics is necessary to quantitatively relate airplane dynamic properties to many task-oriented design requirements. Many such requirements are closed loop in that they involve the pilot as an active controller. Others involve the pilot intermittently as a controller or decision maker. The Flying Qualities Group has an effort planned to develop closed loop criteria to consider future piloting requirements more directly. Both the development of these requirements and their application will require identification and analysis of the pilot's dynamics and workload.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Relationship of the Flying Qualities Specification to Task Performance


    Beteiligte:
    F. L. George (Autor:in) / D. J. Moorhouse (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Airplane flying qualities specification revision

    CHALK, C. / WILSON, R. | AIAA | 1968



    Perspectives of the flying qualities specification

    FULLER, S. / MOORHOUSE, D. | AIAA | 1982


    EFA Flying Qualities Specification and its Utilisation

    Marchand, M. / Kochler, R. / Duda, H. et al. | British Library Conference Proceedings | 1994


    EFA Flying Qualities Specification and Its Utilisation

    M. Marchand / R. Koehler / H. Duda et al. | NTIS | 1994